Return-Path: Sender: (Marvin Kaye) To: lml Date: Sun, 30 Jun 2002 16:49:22 -0400 Message-ID: X-Original-Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 4.0b4) with ESMTP id 1530301 for lml@lancaironline.net; Sun, 30 Jun 2002 14:10:04 -0400 Received: from snipe.mail.pas.earthlink.net ([207.217.120.62]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Sun, 30 Jun 2002 14:04:00 -0400 Received: from sdn-ap-007watacop0432.dialsprint.net ([65.176.65.178] helo=f3g6s4) by snipe.mail.pas.earthlink.net with smtp (Exim 3.33 #2) id 17Oj97-0002cp-00 for lancair.list@olsusa.com; Sun, 30 Jun 2002 11:10:02 -0700 X-Original-Message-ID: <001f01c220c5$d9cf8fe0$b241b041@f3g6s4> Reply-To: "Dan Schaefer" From: "Dan Schaefer" X-Original-To: "Lancair list" Subject: Re: First Flight Engine Testing? X-Original-Date: Sun, 30 Jun 2002 23:09:23 -0700 MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 5.50.4133.2400 X-MimeOLE: Produced By Microsoft MimeOLE V5.50.4133.2400 The only major draw-back to much relatively low power, low load ground running of a fresh engine, particularly if it's got chrome jugs, is you run the real risk of glazing the cylinder walls and it'll almost never break-in (how much is much? I don't know). Even a factory fresh engine with either plain steel or Nitrided steel jugs needs to be run sorta hard initially to insure adequate combustion pressures (high power and loaded) to force the compression ring(s) to seat properly. (Check with any good book on aircraft engines for an explanation of how the compression rings - particularly the first one, if there is more than one in your engine, work). This is one of the real "Catch 22's" for the home builder unless you can take advantage of a service like Jack Kane's. I once flew a friend's Piper 6 - 300 that had just had the engine overhauled with chrome cylinders. We were instructed to tow the airplane to the take-off end of the runway, let the tower know what we were doing so they wouldn't delay take-off, start up and take no more than a minute to check mags and prop and full power and then GO! I wasn't comfortable but we used a 10,000 foot runway so we could abort with plenty (?!) of room if needed. After running at near max. power for a couple of hours (with some power changes to keep the CHT's corralled), we reverted to a more normal procedure, though it was recommended that the engine be run hard until oil consumption started to stabilize, which took near 5 -6 hours, with complete stabilization in about 20. So, if your fresh engine has Orange paint smeared on the jugs somewhere (the code for Chrome if memory serves - AP's help out here), beware of very much, if any, low power run-ups - or you're looking at some premature cylinder work. Dan Schaefer